Cold spray nozzles

Abstract

A nozzle assembly for a cold spray deposition system includes a nozzle body with an axial bore. The axial bore defines a converging segment, a diverging segment downstream of the converging segment, and a throat fluidly connected between the converging and diverging segments of the axial bore. A particulate conduit is fixed within the axial bore and extends along the axial bore diverging segment for issuing solid particulate into the diverging segment of the axial bore.

Claims

1. A nozzle assembly for a cold spray system, comprising: a nozzle body with an axial bore, the axial bore defining: a converging segment having a progressively narrowing flow area; a diverging segment downstream of the converging segment; a throat fluidly connected between the converging and diverging segments; a particulate conduit fixed within the axial bore by an insert located in the narrowing flow area of the converging segment, the particulate conduit extending along the axial bore into the diverging segment for issuing solid particles into the diverging segment of the axial bore; and wherein the insert has a plurality of flow apertures that interrupt the narrowing flow area of the converging segment of the nozzle assembly.

2. An assembly as recited in claim 1, wherein the particulate conduit includes an outlet disposed in the diverging segment.

3. An assembly as recited in claim 2, wherein the particulate conduit defines a substantially uniform flow area within both the diverging and converging segments of the axial bore.

4. An assembly as recited in claim 1, wherein the nozzle body includes a steel material.

5. An assembly as recited in claim 1, further including a motive gas coupling connected to the particulate conduit.

6. An assembly as recited in claim 5, wherein the motive gas coupling is a first motive gas coupling, and further including a second motive gas coupling connected to the converging segment of the axial bore.

7. An assembly as recited in claim 1, wherein the insert includes an annulus and a plurality ligaments, the annulus circumferentially surrounding the particulate conduit and the plurality of ligaments extending radially from the annulus.

8. An assembly as recited in claim 7, wherein the plurality of ligaments define circumferentially between one another a plurality of a motive gas flow apertures conforming to the profile of the axial bore.

9. An assembly as recited in claim 1, wherein the particulate conduit has an exterior surface bounding a central portion of the axial bore.

10. An assembly as recited in claim 1, wherein the particulate conduit includes an exterior surface, wherein at least a portion of the exterior surface disposed within the converging segment includes thermal insulation.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) So that those skilled in the art to which the subject disclosure appertains will readily understand how to make and use the devices and methods of the subject disclosure without undue experimentation, embodiments thereof will be described in detail herein below with reference to certain figures, wherein:

(2) FIG. 1 is a schematic view of an exemplary embodiment of a cold spray system constructed in accordance with the present disclosure, showing a cold spray nozzle assembly;

(3) FIG. 2 is a schematic cross-sectional elevation view of the cold spray nozzle assembly of FIG. 1, showing a particulate conduit fixed within the cold spray nozzle assembly;

(4) FIG. 3 is a cross-sectional end view taken along a flow axis of the cold spray nozzle shown in FIG. 1, showing an insert fixing a particulate conduit within the nozzle assembly;

(5) FIG. 4 is a process flow diagram of a method of cold spray deposition in accordance with the present disclosure, showing method operations, and

(6) FIG. 5 is a process flow diagram of a method of making a nozzle for a cold spray deposition process.

DETAILED DESCRIPTION OF THE DISCLOSURE

(7) Reference will now be made to the drawings wherein like reference numerals identify similar structural features or aspects of the subject disclosure. For purposes of explanation and illustration, and not limitation, a partial view of an exemplary embodiment of a cold spray nozzle assembly in accordance with the disclosure is shown in FIG. 1 and is designated generally by reference character 100. Other embodiments of cold spray nozzles, cold spray systems, and methods of cold spray deposition in accordance with the disclosure, or aspects thereof, are provided in FIGS. 2-4, as will be described. The systems and methods described herein can be used for cold gas dynamic spraying (e.g. cold spray), such as for developing depositions of solid particulate on gas turbine engine components.

(8) As shown in FIG. 1, a cold spray deposition system 10 is shown schematically. Cold spray deposition system 10 includes a cold spray nozzle assembly 100, a first motive gas source 12, a second motive gas source 14, and a solid particulate source 16. Cold spray nozzle 100 includes a nozzle body 102 with a first motive gas coupling 104 and a second motive gas coupling 106. First motive gas coupling 104 connects first motive gas source 12 to nozzle body 102. Solid particulate source 16 connects between first motive gas source 12 and first motive gas coupling 104 thereby placing first motive gas source 12 and solid particulate source 16 in fluid communication with cold spray nozzle assembly 100. Second motive gas coupling 106 connects to second motive gas source 14 and places second motive gas source 14 in fluid communication with cold spray nozzle assembly 100.

(9) First motive gas source 12 is configured and adapted to provide first motive gas flow A to cold spray nozzle assembly 100. Solid particulate source 16 introduces solid particulate 18 into first motive gas flow A. First motive gas flow A entrains the introduced solid particulate 18 and conveys the material to cold spray nozzle assembly 100 via first motive gas coupling 104. In embodiments, first motive gas flow A is an inert gas such as nitrogen, helium, argon, or any other gas suitable for conveying solid particulate 18.

(10) Second motive gas source 14 is configured and adapted to provide a second motive gas flow B to cold spray nozzle assembly 100. Cold spray nozzle assembly 100 increases the velocity of second motive gas flow B as it traverses the assembly and prior to introducing first motive gas flow A with entrained solid particulate 18 into second motive gas flow B. Upon introduction, second motive gas flow B accelerates the solid particulate 18 such that solid particulate 18 issues from cold spray nozzle assembly 100 at velocities suitable for developing a deposition 22 on a target substrate 20 of predetermined quality (e.g. consistency). The issuing solid particulate 18 impacts target 20, bonds with a surface opposite cold spray nozzle assembly 100, and forms a deposition 22 on the surface.

(11) With reference to FIG. 2, cold spray nozzle assembly 100 is shown schematically. Cold spray nozzle assembly 100 is configured and adapted for receiving first motive gas flow A with entrained solid particulate 18 and second motive gas flow B. Cold spray nozzle assembly 100 is also configured and adapted for inducing first motive gas flow A with entrained solid particulate 18 at a point in the axial bore where second motive gas flow B has a predetermined pressure, temperature, and velocity different from that of second motive gas flow B at second motive gas flow coupling 106. In embodiments, cold spray nozzle assembly 100 is a converging-diverging nozzle. In certain embodiments, cold spray nozzle assembly is a de Laval nozzle constructed from steel, ceramic, cermet, a polymer material, or a combination thereof. It is contemplated that solid particulate 18 can be a material with a relatively low melting point, such as aluminum.

(12) Cold spray nozzle assembly 100 includes nozzle body 102, a particulate conduit 108, and an insert 140 for fixing particulate conduit 108 within nozzle body 102. Nozzle body 102 defines within its interior an axial bore 110 extending along a particulate flow axis F. Axial bore 110 includes a converging segment 112, a throat 114, and a diverging segment 116. Converging segment 112 is connected to second motive gas coupling 106 and defines a progressively narrowing flow area extending between a relatively large flow area 122 to a relatively small flow area in throat 114, i.e., between upstream and downstream ends of converging segment 112. Diverging segment 116 is in fluid communication with converging segment 112 and is separated from converging segment 112 by throat 114. Throat 114 is fluidly connected between converging segment 112 and diverging segment 116. A flow area defined by diverging segment 116 progressively widens between throat 114 and a nozzle body outlet 124, i.e., between upstream and downstream ends of diverging segment 116.

(13) Particulate conduit 108 is received within nozzle body 102 and extends along a portion of flow axis F. Particulate conduit 108 includes a first end 130 with an inlet 132, midsection 134, and a second end 136 with an outlet 138. First motive gas coupling 104 connects to first end 130 and is in fluid communication with inlet 132. Midsection 134 connects between first end 130 and second end 136, extends through throat 114, and connects inlet 132 in fluid communication with outlet 138. Particulate conduit 108 is disposed within axial bore 110 such that at least portion of first end 130 including inlet 132 is disposed within converging segment 112 and at least a portion of second end 136 including outlet 138 is disposed within diverging segment 116. In embodiments, particulate conduit 108 includes a steel or ceramic material. In certain embodiments, a thermal insulator 150 is disposed over at least a portion of particulate conduit 108 within converging segment 112. Thermal insulator coating 150 can be formed from a ceramic material, such as aluminum oxide for example. This can reduce heat transfer from second motive gas flow B into first motive gas flow A, potentially allowing for higher second motive gas flow B temperatures in converging segment 112 and commensurate higher solid particulate 18 velocities in diverging segment downstream of outlet 138 than possible with conventional nozzles. It is to be understood and appreciated that, in certain embodiments, particulate conduit 108 can be disposed within the axial bore such that output 138 is disposed within converging segment 112 of axial bore 104.

(14) With reference to FIG. 3, insert 140 is shown in an end view. Insert 140 seats within axial bore 110 and fixes particulate conduit 108 therein. In the illustrated embodiment a central annular portion 142 defines a central aperture 144 that surrounds an axially extending portion of particulate conduit surface 118. A plurality of radial ligaments 146 extend from central annular portion 142 and engage an interior surface 126 thereby fixing particulate conduit 108 within axial bore 110. Circumferentially adjacent radial ligaments 146 define between one another flow apertures 148. Insert flow apertures 148 allow second motive gas flow B to traverse insert 140 and are suitably shaped to allow pressure increase, temperature increase, and velocity of second motive gas flow B.

(15) In certain embodiments, insert flow apertures 148 interrupt the otherwise progressive flow area reduction and the flow area of the nozzle within the converging segment of the nozzle. In this respect they interrupt the flow by presenting a relative abrupt reduction in flow area. However, by positioning insert 140 upstream of throat 114 such that the flow area of the apertures 148 is greater than that of throat 114, first motive gas flow A immediately thereafter enters a relatively larger flow area, and continues an otherwise orderly acceleration to throat 114. In embodiments, a plurality of inserts 140 seat within axial bore 110 and fix particulate conduit 108 therein. In certain embodiments, the plurality of inserts 140 are disposed only within converging segment 112. It is to be understood and appreciated that the plurality of inserts can be disposed only within diverging segment 116 or within both converging segment 112 and diverging segment 116, as suitable for an intended application. It is also to be understood and appreciated that, in accordance with certain embodiments, insert 140 can be disposed within throat 114.

(16) With reference to FIG. 4, a cold spray method 200 is shown. As illustrated with a box 210, method 200 includes receiving a first motive gas with entrained solid particulate within a particulate conduit, e.g. particulate conduit 108, fixed within an axial bore, e.g., axial bore 110, of a cold spray nozzle, e.g. cold spray nozzle 100. Method 200 also includes receiving a second motive gas within a converging segment, e.g., converging segment of the axial bore 112, as illustrated with a box 220. In embodiments, only the first motive gas flow includes entrained solid particulate material. Method 200 further includes directing the first motive gas with entrained solid particulate to a diverging segment of the axial bore, e.g., diverging segment 116, as illustrated in a box 240. Method 250 additionally includes for directing the second motive gas to the diverging segment separately from the first motive gas with entrained particulate, as illustrated with a box 250. This allows for conveying the solid particulate through the converging segment of the nozzle without exposing the solid particulate to the temperature, pressure, and velocity changes included by the geometry of the converging segment of the nozzle.

(17) Method 200 includes introducing the first motive gas with entrained solid particulate into the second motive gas flow in the diverging segment of the axial bore, as illustrated with a box 270. Optionally, method 200 can also include for increasing velocity of the second motive gas within the diverging segment prior to the introducing operation, as illustrated with a box 260. In certain embodiments, method 200 optionally includes cooling at least a portion of the particulate conduit disposed in the converging segment of the axial bore using the first motive gas, as illustrated with a box 230.

(18) With reference to FIG. 5, a method 300 of making a nozzle for a cold spray process, e.g., cold spray nozzle 100, is shown. As illustrated with a box 310, method 300 includes determining at least one of a first motive gas flow parameter, e.g., first motive gas flow A, within a cold spray nozzle, e.g. cold spray nozzle 100. Method 300 also includes determining an offset distance D (shown in FIG. 2) between an outlet of a particulate conduit in view of the determined first motive gas flow parameter, e.g., outlet 138, and a throat of the cold spray nozzle, e.g., throat 114, as illustrated with a box 320. Method 300 further includes positioning the particulate conduit axially within the nozzle such that the outlet is axially offset from the throat by the offset distance, as illustrated with a box 330.

(19) In embodiments, offset distance D can be a negative value, indicating the outlet need be disposed upstream of the nozzle throat and within the converging portion of the nozzle to obtain a predetermined deposition characteristic. In certain embodiments, offset distance D can be a positive value, indicating the outlet need be disposed upstream of the nozzle throat and within the converging portion of the nozzle to obtain a predetermined deposition characteristic. It is also contemplated that offset distance D can be zero, indicated that the outlet need be disposed within the nozzle throat.

(20) Cold spray deposition processes using materials like aluminum generally require nozzles constructed from plastic due to the tendency of the material to adhere to the nozzle surfaces defining the bore, potentially fouling the nozzle and disturbing the flow characteristics of the nozzle. While suitable for their intended purpose, such conventional cold spray nozzles can impose temperature limits on the motive gas used to convey the solid particulate through the nozzle. This can limit the velocity of solid particulate, potentially influencing the quality of the deposition developed by the cold spray nozzle. Introducing solid particulate into the converging segment of a conventional nozzle can enable the solid particulate to erode the inner surfaces of the nozzle. This can change flow characteristics of the nozzle and particulate issue velocity, potentially influencing the properties of the particulate deposition.

(21) In embodiments, directing the first and second gases through the axial bore separately allows for changing the properties of the second motive gas according to the bore geometry without influencing the properties entrained solid particulate in the first motive gas flow. This potentially provides higher solid particulate velocities than ordinarily possible using a conventional nozzle.

(22) In certain embodiments, directing the first motive gas with entrained solid particulate through the particulate conduit allows for the use of materials typically not included in conventional cold spray nozzles. For example, since certain types of solid particulate, e.g., aluminum, tend to adhere to steel or carbide surfaces nozzle interior surfaces, flow surfaces within conventional cold spray nozzles typically include a polymer material bounding the nozzle flow path. Directing the first motive gas with entrained particles through the particulate conduit separates the solid particulate from the nozzle body, thereby limiting contact between the solid particulate and nozzle flow path boundary surfaces. This reduces the likelihood of fouling within the cold spray nozzle. For similar reasons, use of the particulate conduit also reduces the tendency of the solid particulate to erode the nozzle interior surfaces.

(23) Analysis by the Applicants indicates that solid particulate injected along the axial bore axis in the diverging segment, in embodiments, will not significantly impact the walls. This could prevent fouling of a steel nozzle in the diverging segment where intermixing the first and second gas flows would ordinarily suggest solid particulate would contact the nozzle flow surfaces, for example. In embodiments, this potentially allows for running the cold spray nozzle with temperatures exceeding 800 degrees Celsius (about 1500 degrees Fahrenheit) as solid particulate issues from the particulate conduit into the diverging segment at region where the second motive gas flow has cooled to about 500 degree Celsius (about 900 degrees Fahrenheit). It is contemplated that, in accordance with certain embodiments, the cold spray nozzle could have a plastic end portion coupled to metal, cermet, or ceramic nozzle body portion to further reduce the likelihood of fouling in the diverging segment of the axial bore.

(24) The methods and systems of the present disclosure, as described above and shown in the drawings, provide for cold spray deposition nozzles, systems and methods with superior properties including increased issue velocity. While the apparatus and methods of the subject disclosure have been shown and described with reference to the disclosed embodiments, those skilled in the art will readily appreciate that changes and/or modifications may be made thereto without departing from the scope of the subject disclosure.